Type Acceptance Report

Transcription

1 TAR 18/21B/5 SOCATA TB Series Aircraft Certification Unit

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3 TABLE OF CONTENTS EXECUTIVE SUMMARY 1 1. INTRODUCTION 1 2. AIRCRAFT CERTIFICATION DETAILS 2 3. APPLICATION DETAILS AND BACKGROUND INFORMATION 5 4. NZCAR DATA REQUIREMENTS 6 5. NEW ZEALAND OPERATIONAL RULE REQUIREMENTS 10 ATTACHMENTS 11 APPENDIX 1 11 i TAR 18/21B/5 SOCATA TB Series

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5 Executive Summary New Zealand Type Acceptance has been granted to the SOCATA TB9/10/20/21/200 Series based on validation of Type Certificate number EASA.A.378. There are no special requirements for import. This report covers all the Models and serial numbers currently listed on the EASA Type Certificate, which are now eligible for the issue of an Airworthiness Certificate in the Standard Category in accordance with NZCAR , subject to any outstanding New Zealand operational requirements being met. (See Section 5 of this report for a review of compliance of the basic type design with the operating Rules.) Subsequent models or serial numbers approved under the EASA type certificate can become type accepted after supply of the applicable documentation, in accordance with the provisions of NZCAR 21.43(c). NOTE: The information in this report was correct as at the date of issue. The report is generally only updated when an application is received to revise the Type Acceptance Certificate. For details on the current type certificate holder and any specific technical data, refer to the latest revision of the State-of-Design Type Certificate Data Sheet referenced herein. 1. Introduction This report details the basis on which Type Acceptance Certificate No. 18/21B/5 was granted in the Standard Category in accordance with NZCAR Part 21 Subpart B. Specifically the report aims to: (a) Specify the foreign type certificate and associated airworthiness design standard used for type acceptance of the model(s) in New Zealand; and (b) Identify any special conditions for import applicable to any model(s) covered by the Type Acceptance Certificate; and (c) Identify any additional requirements which must be complied with prior to the issue of a NZ Airworthiness Certificate or for any subsequent operations. The report also notes the status of all models included under the State-of-Design type certificate which have been granted type acceptance in New Zealand. Models covered by the type acceptance certificate issued under Part 21B are listed in Section 2 of this report. Models which were certificated prior to that under NZCAR Section B.9 and are type accepted under the transitional arrangements of Part 21 Appendix A(c) are listed in Appendix 1. 1 TAR 18/21B/5 SOCATA TB Series

6 2. Aircraft Certification Details (a) State-of-Design Type and Production Certificates: Manufacturer: SOCATA EADS SOCATA (2000 to 2009) Société de Construction d'avions de Tourisme et d'affaires SOCATA - Groupe AEROSPATIALE (1979 to 2000) Type Certificate: EASA.A.378 European Aviation Safety Agency Production Approval: JAR21 No. F.G.027 (b) Models Covered by the Part 21B Type Acceptance Certificate: (i) Model: TB10 MCTOW: 2535 lb. [1150 kg] Max. No. of Seats: 5 Noise Standard: ICAO Annex 16 Engine: Lycoming O-360-A1AD Type Certificate: E-286 Propeller: Hartzell HC-C2YK-1BF/F7666A-2 Type Certificate: P-920 (ii) Model: MCTOW: TB lb. [1060 kg] Max. No. of Seats: 5 Noise Standard: ICAO Annex 16 Engine: Lycoming O-320-D1A or D2A Type Certificate: E-274 Propeller: Sensenich 74DM6 S8 061 or 054 or 058 Type Certificate: P-886 Propeller: Hartzell HC-C2YL-1BF/F7663A-4 Type Certificate: P-920 TAR 18/21B/5 SOCATA TB Series 2

7 (iii) Models: TB20 MCTOW: 2943 lb. [1335 kg] Aircraft without modification lb. [1400 kg] Max. No. of Seats: 5 Noise Standard: ICAO Annex 16 Engine: Type Certificate: Lycoming IO-540-C4D5D or B5D 1E4 Propeller: Hartzell HC-C2YK-1BF/F8477A-4 Type Certificate: P-920 Propeller: Type Certificate: Hartzell HC-C3YR-1RF/F7693F or FB (OPT ) P25EA (iv) Models: MCTOW: TB lb. [1400 kg] Max. No. of Seats: 5 Noise Standard: ICAO Annex 16 Engine: Type Certificate: Lycoming TIO-540-AB1AD E14EA Propeller: Hartzell HC-C2YK-1BF/F8477A-4 Type Certificate: P-920 Propeller: Type Certificate: Hartzell HC-C3YR-1RF/F7693F or FB (OPT ) P25EA 3 TAR 18/21B/5 SOCATA TB Series

8 (v) Models: MCTOW: TB lb. [1150 kg] Max. No. of Seats: 5 Noise Standard: ICAO Annex 16 Engine: Type Certificate: Lycoming IO-360-A1B6 1E10 Propeller: Hartzell HC-C2YK-1BF/F7666A-2 Type Certificate: P-920 NOTE: See Advisory Circular AC21-1 Appendix 2 for the New Zealand type acceptance status of engines and propellers listed above. TAR 18/21B/5 SOCATA TB Series 4

9 3. Application Details and Background Information The application for New Zealand type acceptance of the TB20 GT serial number range was from the importer, dated 17 July The first-of-type example was serial number 2053, registered as ZK-SOC. The TB Series is a four-seat low-wing single-engined light aircraft of all-metal semi-monococque construction. Type Acceptance Certificate Number 18/21B/5 was granted on 13 September 2017 to all the SOCATA TB Series that were not already type accepted, based on validation of Type Certificate EASA.A.378. There are no special requirements for import into New Zealand. The 180 hp TB10 Tobago was the first model in the all-new TB Caribbean series developed by SOCATA in the late 1970s to replace the Rallye family. The TB9 Tampico was a cheaper version for the flight training market, with a160 hp engine, smaller fuel tanks, 4-ply tyres and different seats, and could be had with a fixed-pitch propeller. The TB20 Trinidad was a touring version with a 250 hp 6-cylinder engine and retractable undercarriage. Other changes included the wing dihedral increased to 6.5º, different profile on the aileron leading edge, electric wing flaps operating mechanism, larger horizontal stabiliser and a trim tab for the rudder, and increased fuel tanks capacity. The TB21 Trinidad TC was the same aircraft except for a turbocharged engine. The TB200 was a development of the TB10 with 200 hp fuel-injected engine. The models share a common fuselage, wing and empennage and no distinction is drawn between the airframes so that the variants all co-exist within the same run of serial numbers. The TB Series were modernised in 2000 including a change to a 28 volt electrical system, and were known as Generation Two. This applies to serial numbers 948 and later, plus S/N 823 to 849 and S/N 888. The marketing designation GT was added to the model names. GT versions have a bigger cabin and aerodynamic improvements, including shaped wing tips and vertical stabiliser. The rear windows are also more blended with the fuselage. The first example of the TB Series on the New Zealand register was a TB9 which was registered ZK-TBA in 1982, while the first TB10s were ZK-MBR and ZK-MBS in The first examples of the TB20 were ZK-JFC followed by ZK-JCC, both in TAR 18/21B/5 SOCATA TB Series

10 4. NZCAR Data Requirements The type data requirements of NZCAR Part 21B Para have been satisfied by supply of the following documents, or were already held by the CAA: (1) State-of-Design Type certificate: EASA Type Certificate Data Sheet number A.378 at Issue 03 dated 6 October 2010 Model TB10 approved April 26, 1979 Model TB9 approved September 27, 1979 Model TB20 approved December 18, 1981 Model TB21 approved May 23, 1985 Model TB200 approved October 30, 1991 This supersedes the original type certificate: DGAC Certificat de Navigabilité de Type Numéro 165 SOCATA TB Series DGAC Fiche de Navigabilité No. 165 SOCATA Avions (2) Airworthiness design requirements: (i) Airworthiness Design Standards: The certification basis of the SOCATA TB Series is FAR Part 23, including Amendments 23-1 through Two exemptions were granted for the TB9 and TB10, and one special condition applied to the TB21, which have been reviewed and accepted by the CAA. This is an acceptable certification basis in accordance with NZCAR Part 21B Para 21.41, because FAR Part 23 is the basic standard for Normal Category Airplanes called up under Part 21 Appendix C. There are no non-compliances and no additional special conditions have been prescribed by the Director under (ii) Special Conditions: TB20: FAR at Amendment Because the landing gear is being held in the retracted position by hydraulic pressure alone, some requirements are modified as follows: in landing gear extension is checked up to V NO, and in (a) the airspeed 1.6 V SI is replaced by V NO. (iii) Equivalent Level of Safety Findings: Nil (iv) DGAC Exemptions: TB9 and TB10: FAR (a)(2) A slight roll instability of the aircraft in the landing configuration during a go-around was accepted on the basis that the pilot is closely monitoring this phase of flight. FAR (f) The Labinal anti-collision light intensity with red glass optic lense is slightly less than that required by the regulation. (v) Airworthiness Limitations: See the DGAC-Approved Chapter 4 Airworthiness Limitations in the AMM TAR 18/21B/5 SOCATA TB Series 6

11 (3) Aircraft Noise and Engine Emission Standards: (i) Environmental Standard: The Model TB10 was certificated for noise against the French Decree dated April 15, 1977, and ICAO Chapter X, Appendix 6, Annex 16. For subsequent TB Models the French Decree at later dates and FAR Part 36 Appendix G were added. (ii) Compliance Listing: See the TCDS Section _.V Notes Note 1 Approved Noise Levels. (4) Certification Compliance Listing: TB9 General Description BE/EG No. 136/79 RJ/JD Issue 1 TB9 No. 9 Compte-Rendu des Essais en Vol R.EV/TB No. 5/79 CL/SC TB9 Safety Margins for the Structure BE/EG No 248/79 YV/PL Issue Nr 2 TB10 Aircraft: General Description BE/EG No. 66/79 RJ/JD Issue Nr 6 TB10 Note TB Fatigue Life Assessment TB/I No. 7/78 YC/PL TB10 Safety Margins for the Structure BE/EG No. 140/79 YC/PL TB20 Description of Model (from s/n 731) BE/EG No. 203/80 RJ/PL TB20 Recapitulative File of Safety Margins for the Structure BE/EG No. 326/80 TB Aircraft Fatigue Tests Report EG No.278/85 RJ October 1985 (Summary of TB10 Fatigue Tests, Extrapolation of results to TB20 and TB21) In-Flight Test Report Compliance with Airworthiness Regulations FAR Part 23 Amendment 16 included - Certification of the TB20 Airplane R. EV/TB 4/81 FAR-23 Amendment 16 - Compliance Check-List - TB-9 "Tampico", TB-10 "Tobago", TB-20 "Trinidad" BE/EG No. 60/83 RJ/PL Edition 7 January 1989 (5) Flight Manual: French DGAC-Approved Airplane Flight Manual or Pilot's Operating Handbook, including EASA-Approved revision and temporary revisions, with model and serial number applicability as follows: Model: Serial Number Range: Part Number: CAA No.: TB9: S/N 1 to S/N 730 Z AIR 2174 TB9: S/N 731 to S/N 878 (except S/N 765) Z AIR 3455 TB9: S/N 879 to S/N 947 (plus S/N 765) Z AIR 3456 TB9: S/N 948 and up Z00.DUDFM00EE3R2EN AIR 3457 TB9: S/N 948 and up (with Mod.139) GT Z E4R1 AIR 3458 TB10: S/N 1 to S/N 730 Z R2 AIR 3459 TB10: S/N 731 to S/N 822 (except S/N*) Z R2 AIR 3460 TB10: S/N 823 to S/N 947 (plus S/N*) Z R2 AIR 2499 TB10: S/N 948 and up GT Z E3R7 AIR 2395 S/N * is (S/N 840, 807, 808 and S/N 816 to s/n 819) 7 TAR 18/21B/5 SOCATA TB Series

12 TB20 S/N 1 to S/N 587 (without Kit.9118) Z AIR 2417 TB20 S/N 588 to S/N 730 (plus S/N 1 to S/N Z AIR with Kit.9118 [mod.50]) TB20 S/N 731 to 878 (except 823 to 849) Z AIR 2416 TB20 S/N 879 to S/N 947 (except S/N 888) Z AIR 3462 TB20 S/N 948 and up (plus S/N 823 to 849 Z E2R11 AIR 3387 and 888) GT TB21: S/N 1 to S/N 730 Z AIR 3463 TB21: S/N 731 to S/N 878 Z R2 AIR 3464 TB21: S/N 879 to S/N 947 Z R1 AIR 3465 TB21: S/N 948 and up GT Z E2R6 AIR 3466 TB200: S/N 1 and up Z E0R6 AIR 3467 (6) Operating Data for Aircraft: (i) Maintenance Manual: TB9 Maintenance Manual Part Number Z E0R19 TB10 Maintenance Manual Part Number Z E0R19 TB20 Maintenance Manual Part Number Z E0R19 TB21 Maintenance Manual Part Number Z E0R19 TB (14 Volt) Electrical Maintenance Manual P/N Z E0R6 TB Generation Two (28V) Wiring Manual P/N Z E0R3 TB20-21 (14 Volt) Electrical Maintenance Manual Part No, Z E0R5 TB20-21 Generation Two (28V) Wiring Manual Part No. Z E0R3 (ii) Current service Information: Service Bulletins Service Letters SOCATA Information Bulletins (I.B.) SOCATA Information (S.I.) (iii) Illustrated Parts Catalogue: TB9 Standard IPC Part Number Z E0R17 TB10 Standard IPC Part Number Z E0R17 TB20 Standard IPC Part Number Z E0R17 TB21 Standard IPC Part Number Z E0R17 (7) Agreement from manufacturer to supply updates of data in (5), and (6): SOCATA provides CAA access to publications at TAR 18/21B/5 SOCATA TB Series 8

13 (8) Other information: TB9 Standard and Optional Equipment List BE/EQ No. 233/79 Issue Nr 3 Electrical Load Analysis IFR TB9 Aircraft BE/EQ No 255/79 ET/PL TB9/TB10 List of Equipment NAV No.232/89-RJ Issue No.7 January Volt Electrical Power From S/N 948 TB10 Standard and Optional Equipment List BE/EG No. 74/79 Issue Nr 4 Electrical Load Analysis IFR TB10 Aircraft BE/ED No. 183/78 ET/PL TB20 List of Equipment NAV No. 92/89 RJ Issue No.8 January 2005 (28-Volt Electrical Power, S/N , 888 and 948 up) Electrical Load Analysis TB20 28 VDC Generation BE/EQ No. 285/88 9 TAR 18/21B/5 SOCATA TB Series

14 5. New Zealand Operational Rule Compliance Compliance with the retrospective airworthiness requirements of NZCAR Part 26 has been assessed as they are a prerequisite for the grant of an airworthiness certificate. CAR Part 26: Subpart B Additional Airworthiness Requirements Appendix B All Aircraft PARA: REQUIREMENT: MEANS OF COMPLIANCE: B.1 Marking of Doors and Emergency Exits To be determined on an individual aircraft basis B.2 Crew Protection Requirements CAM 8 Appdx. B #.35 Not Applicable Agricultural Aircraft only Compliance with the following additional NZ operating requirements has been reviewed and were found to be covered by either the original certification requirements or the basic build standard of the aircraft, except as noted: CAR Part 91: Subpart F Instrument and Equipment Requirements PARA: REQUIREMENT: MEANS OF COMPLIANCE: Seating and Restraints Safety belt/shoulder Harness FAR Pax Information Signs Smoking, safety belts fastened Not Applicable Less than 10 passenger seats Min. VFR (1) ASI (2) Machmeter (3) Altimeter (4) Magnetic Compass (5) Fuel Contents (6) Engine RPM (7) Oil Pressure FAR (a) N/A No Mach limitations FAR (b) FAR (c) FAR (a) FAR (d) FAR (b) (8) Coolant Temp (9) Oil Temperature (10) Manifold Pressure (11) Cylinder Head Temp. (12) Flap Position (13) U/c Position (14) Ammeter/Voltmeter N/A Air cooled engine fitted FAR (c) FAR (h) FAR (f) FAR (a)(2) N/A or FAR (e) FAR Night VFR Instruments and Equipment Operational requirement Compliance as applicable VFR Communication Equipment Operational requirement Compliance as applicable IFR Instruments and Equipment Operational requirement Compliance as applicable IFR Communication and Navigation Equipment Operational requirement Compliance as applicable Emergency Equipment: (a) More Than 9 pax First Aid Kits per Table 7 Fire Extinguishers per Table 8 (b) More than 20 pax Axe readily accessible to crew (c) More than 61 pax Portable Megaphones per Table 9 Operational Requirement Compliance as applicable Operational Requirement Compliance as applicable Not Applicable Less than 20 passenger seats Not Applicable Less than 61 passenger seats ELT TSO C MHz after 22/11/2007 Operational requirement Compliance as applicable Oxygen Indicators Volume/Pressure/Delivery Operational requirement Compliance as applicable Oxygen for non-pressurised Aircraft Operational requirement Compliance as applicable SSR Transponder and Altitude Reporting Equipment Operational requirement Compliance as applicable Altitude Alerting Device Turbojet or Turbofan Not Applicable Not turbo jet or turbofan powered Assigned Altitude Indicator Operational requirement Compliance as applicable A.15 ELT Installation Requirements To be determined on an individual aircraft basis CAR Part 135: Subpart F Instrument and Equipment Requirements PARA: REQUIREMENT: MEANS OF COMPLIANCE: Seating and Restraints Shoulder harness flight-crew seats FAR Additional Instruments (Powerplant and Propeller) FAR Night Flight Landing light, Pax compartment Operational requirement Compliance as applicable IFR Operations Speed, Alt, spare bulbs/fuses Operational requirement Compliance as applicable Emergency Equipment (Part (a) and (b)) Operational requirement Compliance as applicable Cockpit Voice Recorder N/A Only for 2-crew helicopters with more than 10 pax Flight Data Recorder Not Applicable Less than 10 passenger seats Additional Attitude Indicator Not Applicable Not turbo jet or turbofan powered NOTES: 1. A Design Rule reference in the Means of Compliance column indicates the Design Rule was directly equivalent to the CAR requirement, and compliance is achieved for the basic aircraft type design by certification against the original Design Rule. 2. The CAR Compliance Tables above were correct at the time of issue of the Type Acceptance Report. The Rules may have changed since that date and should be checked individually. TAR 18/21B/5 SOCATA TB Series 10

15 Attachments The following documents form attachments to this report: Sign off Three-view drawing SOCATA Model TB20 Trinidad Copy of Type Certificate Data Sheet Number EASA.A David Gill Team Leader Airworthiness... Checked Craig Bamber Airworthiness Engineer Appendix 1 List of Type Accepted Variants: Model: Applicant: CAA Work Request: Date Granted: TB9 AC /NZCAR Part 21 Appendix A(c) TB10 AC /NZCAR Part 21 Appendix A(c) TB20 AC /NZCAR Part 21 Appendix A(c) TB20 GT, TB21, TB200 H Bechgaard 18/21B/5 13 September TAR 18/21B/5 SOCATA TB Series